Characterization of Temperature Sensitive Paint for Application in Hypersonic Ludwieg Tubes at the University of Tennessee-Reference-Cited by-同舟云学术

Characterization of Temperature Sensitive Paint for Application in Hypersonic Ludwieg Tubes at the University of Tennessee

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
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Author:

Smith Cary¹,Kreth Phillip A.¹,Schmisseur John D.¹,Strickland Garrett²

Affiliation:

1. The University of Tennessee Space Institute

2. Lockheed Martin

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1660

Reference18 articles.

1. Temperature- and Pressure-Sensitive Paint Measurements in Short-Duration Hypersonic Flow

2. Kurits, I., Lewis, M. J., Hamner, M., and Norris, J. "Continued Development of a Global Heat Transfer Measurement System at AEDC Hypervelocity Wind Tunnel 9," NASA Technical Reports Server. https://ntrs.nasa.gov/citations/20070022279.

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